Methods of making articles having toughened and untoughened regions

a technology of region and hardening, applied in the direction of superimposed coating process, manufacturing tools, liquid/solution decomposition chemical coating, etc., can solve the problems of foreign objects sometimes undetected entering the engine, affecting the overall weight of the article, so as to increase the overall weight and increase the strength
US20100148396A1Active Publication Date: 2010-06-17GENERAL ELECTRIC CO

Patent Information

Authority / Receiving Office
US ยท United States
Patent Type
Applications(United States)
Current Assignee / Owner
GENERAL ELECTRIC CO
Publication Date
2010-06-17

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Abstract

Methods of making an article having at least one toughened region and at least one untoughened region involving providing a material, applying a toughening agent to a portion of the material, shaping the material to produce a preform, applying an untoughened resin to the preform, and curing the preform having the applied untoughened resin to produce the at least one toughened region and the at least one untoughened region wherein the toughened region comprises a toughened resin having a fracture toughness of at least about 1.0 MPa-m1 / 2.
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Description

CROSS REFERENCE TO RELATED APPLICATIONS

[0001] This is a Continuation-in-Part of application Ser. No. 11 / 736,319, filed Apr. 17, 2007, which is herein incorporated by reference in its entirety.TECHNICAL FIELD

[0002] Embodiments described herein generally relate to methods of making articles having toughened and untoughened regions. More particularly, embodiments herein generally describe methods of making articles from composite materials having toughened and untoughened regions.BACKGROUND OF THE INVENTION

[0003] In gas turbine engines, such as aircraft engines, air is drawn into the front of the engine, compressed by a shaft-mounted compressor, and mixed with fuel in a combustor. The mixture is then burned and the hot exhaust gases are passed through a turbine mounted on the same shaft. The flow of combustion gas expands through the turbine, which in turn spins the shaft and provides power to the compressor. The hot exhaust gases are further expanded through nozzles at the back of the en...

Claims

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